Please use this identifier to cite or link to this item:
|Title:||Application of three-dimensional interfaces for data transfer in aeroelastic computations||Authors:||Sadeghi, M.
|Issue Date:||2004||Citation:||Sadeghi, M.,Liu, F.,Lai, K.L.,Tsai, H.M. (2004). Application of three-dimensional interfaces for data transfer in aeroelastic computations. Collection of Technical Papers - AIAA Applied Aerodynamics Conference 2 : 1116-1145. ScholarBank@NUS Repository.||Abstract:||A framework of requirements for fluid-structure interfaces is presented and applied to evaluate the qualities of various transfer methods. The Constant-Volume Tetrahedron approach is compared with an inverse Boundary Element Method, both of which are three-dimensional techniques. Advantages of these three-dimensional interfaces over conventional planar interpolation methods (such as the infinite-plate spline interpolation) are demonstrated and discussed. Comparisons are based on geometric considerations as well as on results from aeroelastic computations. For flutter calculations, the three-dimensional Euler equations are solved by a finite-volume method coupled with a finite-difference method for the modal structural equations. The Constant-Volume Tetrahedron approach is more easily implemented as the inverse Boundary Element Method. However, the application of elastic equilibrium in case of the BEM is more physically meaningful than the arbitrary constraint of a constant elemental volume. A detailed comparison of both approaches in terms of implementation and applicability is provided.||Source Title:||Collection of Technical Papers - AIAA Applied Aerodynamics Conference||URI:||http://scholarbank.nus.edu.sg/handle/10635/111543||ISSN:||10485953|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Sep 6, 2019
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.